Experimental Investigation and Simulation of Electro-Mechanical Behaviour of Hybrid Sandwich Composite Radomes for Aerospace Applications
This paper presents a comprehensive study of the material selection, manufacturing, and Electro-Mechanical testing of radomes made from Polymer Matrix Sandwich Composite materials. The objective is to achieve optimal electromagnetic (EM) and mechanical performance using a combination of PMI foam cor...
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Published in | Mechanics of Advanced Composite Structures Vol. 11; no. 2; pp. 401 - 412 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Semnan University
01.11.2024
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Subjects | |
Online Access | Get full text |
ISSN | 2423-4826 2423-7043 |
DOI | 10.22075/macs.2024.30908.1517 |
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Abstract | This paper presents a comprehensive study of the material selection, manufacturing, and Electro-Mechanical testing of radomes made from Polymer Matrix Sandwich Composite materials. The objective is to achieve optimal electromagnetic (EM) and mechanical performance using a combination of PMI foam core and hybrid face sheets (Kevlar & S Glass) sandwich composite structures. The selection of the material configuration was based on a Multi Criteria Decision Matrix (MCDM) method to meet the requirements of Electromagnetic Interference (EMI) transparency and aerodynamic/inertial loads during flights. A full-scale nose radome was manufactured using a hand-layup technique assisted by vacuum bagging, specifically designed for flight vehicles with speeds up to <0.8 Mach. The EMI behavior of the radome was experimentally tested using the free space measurement method and verified through numerical modeling in Altair FEKO software, which showed minimal EM losses of 3% and <1% respectively. Multiple specimens were prepared to determine the mechanical properties and were tested according to ASTM standards for tensile and flexural properties. Additionally, finite element modeling (FE) was employed to validate the mechanical properties of the radome, ensuring that it meets the required constraints. The combined results from the EMI testing, FE modeling, and mechanical testing provided an optimum combination of materials and structure that satisfies the functional requirements of the radome. |
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AbstractList | This paper presents a comprehensive study of the material selection, manufacturing, and Electro-Mechanical testing of radomes made from Polymer Matrix Sandwich Composite materials. The objective is to achieve optimal electromagnetic (EM) and mechanical performance using a combination of PMI foam core and hybrid face sheets (Kevlar & S Glass) sandwich composite structures. The selection of the material configuration was based on a Multi Criteria Decision Matrix (MCDM) method to meet the requirements of Electromagnetic Interference (EMI) transparency and aerodynamic/inertial loads during flights. A full-scale nose radome was manufactured using a hand-layup technique assisted by vacuum bagging, specifically designed for flight vehicles with speeds up to <0.8 Mach. The EMI behavior of the radome was experimentally tested using the free space measurement method and verified through numerical modeling in Altair FEKO software, which showed minimal EM losses of 3% and <1% respectively. Multiple specimens were prepared to determine the mechanical properties and were tested according to ASTM standards for tensile and flexural properties. Additionally, finite element modeling (FE) was employed to validate the mechanical properties of the radome, ensuring that it meets the required constraints. The combined results from the EMI testing, FE modeling, and mechanical testing provided an optimum combination of materials and structure that satisfies the functional requirements of the radome. |
Author | Muhammad Talha Aamir Zhaib Muneer Ahmed Muhammad Ali Nasir Zafar Iqbal |
Author_xml | – sequence: 1 fullname: Zhaib Muneer Ahmed organization: Department of Mechanical Engineering, University of Engineering & Technology (UET) Taxila, Rawalpindi, Punjab 47050, Pakistan – sequence: 2 fullname: Muhammad Ali Nasir organization: Department of Mechanical Engineering, University of Engineering & Technology (UET) Taxila, Rawalpindi, Punjab 47050, Pakistan – sequence: 3 fullname: Zafar Iqbal organization: School of Chemical & Materials Engineering (SCME), National University of Science & Technology (NUST) Islamabad, Pakistan – sequence: 4 fullname: Muhammad Talha Aamir organization: Department of Mechanical Engineering, University of Engineering & Technology (UET) Taxila, Rawalpindi, Punjab 47050, Pakistan |
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SubjectTerms | electro-mechanical characterisation hybrid sandwich composites mcdm nose radomes |
Title | Experimental Investigation and Simulation of Electro-Mechanical Behaviour of Hybrid Sandwich Composite Radomes for Aerospace Applications |
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